EP2644365B1 - Méthode de moulage RTM - Google Patents

Méthode de moulage RTM Download PDF

Info

Publication number
EP2644365B1
EP2644365B1 EP13173654.8A EP13173654A EP2644365B1 EP 2644365 B1 EP2644365 B1 EP 2644365B1 EP 13173654 A EP13173654 A EP 13173654A EP 2644365 B1 EP2644365 B1 EP 2644365B1
Authority
EP
European Patent Office
Prior art keywords
resin
reinforcing fiber
laminate
mold
evacuation
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP13173654.8A
Other languages
German (de)
English (en)
Other versions
EP2644365A2 (fr
EP2644365A3 (fr
Inventor
Toshihide Sekido
Kazuaki Kitaoka
Hiroshi Odani
S Nishiyama
M Shimizu
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Toray Industries Inc
Original Assignee
Mitsubishi Heavy Industries Ltd
Toray Industries Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from JP2002295933A external-priority patent/JP4104413B2/ja
Priority claimed from JP2002295934A external-priority patent/JP4104414B2/ja
Priority claimed from JP2002312454A external-priority patent/JP4104422B2/ja
Application filed by Mitsubishi Heavy Industries Ltd, Toray Industries Inc filed Critical Mitsubishi Heavy Industries Ltd
Publication of EP2644365A2 publication Critical patent/EP2644365A2/fr
Publication of EP2644365A3 publication Critical patent/EP2644365A3/fr
Application granted granted Critical
Publication of EP2644365B1 publication Critical patent/EP2644365B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/0005—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor using fibre reinforcements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/546—Measures for feeding or distributing the matrix material in the reinforcing structure
    • B29C70/547—Measures for feeding or distributing the matrix material in the reinforcing structure using channels or porous distribution layers incorporated in or associated with the product
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/546—Measures for feeding or distributing the matrix material in the reinforcing structure
    • B29C70/548—Measures for feeding or distributing the matrix material in the reinforcing structure using distribution constructions, e.g. channels incorporated in or associated with the mould
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks

Definitions

  • the present invention relates to improvement of a method of Resin Transfer Molding (hereinafter, referred to as "RTM") for molding a structural material of a fiber reinforced plastic (hereinafter, referred to as "FRP”), and specifically, to a method of RTM molding in which it is possible to mold a thick material, and further, it is possible to improve a quality of surface property or to increase a fiber volume content (hereinafter, also referred to as "Vf”) of an FRP molded material to be molded.
  • RTM Resin Transfer Molding
  • FRP fiber reinforced plastic
  • Vf fiber volume content
  • GB 2316036A discloses a bagging blanket and method for forming an FRP. Further examples of molding methods are provided in JP 2001 064406A , JP 2002 172630A and JP 556 127426A .
  • FRP has been used in various fields, as a method for producing an FRP structural material, general is a so-called prepreg/autoclave molding method wherein, after a preform having a shape of a structural material to be molded is formed beforehand by prepregs, the preform is cured in an autoclave set at a predetermined condition in temperature and pressure.
  • RTM molding is paid attention to in order to reduce the production cost, and this method is developed gradually.
  • Many methods are proposed as RTM molding methods for producing panels and beam materials which are structural members for air planes or architecture requiring high strength, lightweight and low cost or for producing FRP molded products such as outer panels of vehicles.
  • peel plys/resin distribution media are disposed on both surfaces of a reinforcing fiber substrate comprising a laminate of reinforcing fiber materials, the whole thereof is covered with a bag material, and a resin injection gate and an evacuation gate for reducing a pressure are provided relative to the inside covered with the bag material.
  • a resin is injected from the resin injection gate while being reduced in pressure by evacuating the inside of the bag material through the evacuation gate, and basically, the resin is flown from the upper surface side to the lower surface side of the reinforcing fiber substrate, or from the lower surface side to the upper surface side, to impregnate the resin into the reinforcing fiber substrate.
  • the resin is cured at a room temperature or under a heated atmosphere condition, and after curing, the molded product is taken out from the mold by removing the bag material.
  • the permeability corresponds to a distance (thickness) of resin impregnation into the substrate.
  • the above-described resin distribution medium is formed as a member having a relatively large surface irregularity with a low resistance for gas permeation in order to increase the resin distribution property.
  • the resin distribution media having such a relatively large surface irregularity are disposed on both surfaces of the reinforcing fiber substrate and the molding is carried out in this condition, the relatively large surface irregularity of the resin distribution medium is reflected to the design surface which is one surface of the molded product. As a result, the designability is damaged and an irregularity is formed on the surface of the molded product, and therefore, there is a problem that the properties such as aerodynamic property decrease.
  • the degree of the irregularity of the resin distribution medium affects the resin distribution and gas permeation performances
  • the irregularity of the resin distribution medium for improving resin distribution and gas permeation performances (a relatively large irregularity)
  • the irregularity of the resin distribution medium for improving the surface property of the molded product (a relatively small irregularity) are in a relationship opposite to each other. Therefore, in the conventional method wherein substantially same resin distribution media are disposed on both surfaces of a reinforcing fiber substrate, it is difficult to achieve both of increase of the resin impregnation property and improvement of the surface property of a molded product, and it becomes particularly difficult in the molding using a thick reinforcing fiber substrate.
  • a reinforcing fiber substrate is placed on a mold and a resin distribution medium is disposed at a position opposite to the mold, a resin injection port and an evacuation port are disposed, they are covered with a bag material from the upper side, and a matrix resin is injected at a condition where the inside of a cavity is reduced in pressure by evacuation.
  • the flowing-in route of the resin into the substrate is formed as a route in which the resin is distributed mainly from the injection port along the surface direction of the substrate disposed in the mold and the distributed resin is impregnated in the thickness direction of the substrate.
  • the Vf of the reinforcing fibers is, for example, 45% and the gap between reinforcing fibers is relatively great, because the fiber volume content of the final molded product becomes low although a good resin impregnation property can be obtained, only a product having poor strength and lightweight property can be obtained. Namely, the resin impregnation property and the fiber volume content Vf are in a relationship opposite to each other, and it is difficult to achieve both improvement of the resin impregnation property and increase of the fiber volume content together. Moreover, although it is preferred depending on a molded product to control the fiber volume content from the necessity of stabilization of the quality, it is also difficult to satisfy such a requirement.
  • the reinforcing fiber substrate is formed as a laminate of a plurality of reinforcing fiber materials in order to obtain an FRP molded product with a predetermined thickness, as to the thickness direction, that is, as to the direction perpendicular to the lamination surface in the reinforcing fiber material laminate, the resistance against the resin flow is generally high, and there is a limit in the reaching distance of the resin being impregnated in the thickness direction of the substrate.
  • An aim of the present invention is to provide a method of RTM molding (method for producing an FRP) which can solve the above-described various problems in the conventional methods, which can mold even a thick FRP structural material with a good resin impregnation property, and which can realize improvement of the surface quality, increase of the lightweight property and achievement of an excellent strength.
  • a resin is injected into the mold through the resin distribution media to impregnate the reinforcing fiber substrate with the resin injected, is characterized in that a resin flow resistance of a first resin distribution medium placed on a first surface of the reinforcing fiber substrate is set lower than a resin flow resistance of a second resin distribution medium placed on a second surface of the reinforcing fiber substrate, and the evacuation is carried out through the second resin distribution medium while the resin is injected into the first resin distribution medium to impregnate the reinforcing fiber substrate with the resin injected (a first method).
  • the resin flow resistance can be determined by measuring a gas permeation resistance and determining it as a value corresponding to the measured gas permeation resistance.
  • the permeability generally shown by the following equation has the same meaning as that of the resin flow resistance, such a value may be employed.
  • the reinforcing fiber substrate may be a single layer or may be formed as a laminate of a plurality of reinforcing fiber materials
  • the first method of RTM molding is suitable particularly for molding of a thick product, namely, for molding for impregnating a resin into a thick reinforcing fiber substrate
  • the target of the present invention is mainly a case where a reinforcing fiber substrate comprising a laminate of a plurality of reinforcing fiber materials is used.
  • the resin flow resistance of the above-described second resin distribution medium is set lower than the resin flow resistance of the above-described reinforcing fiber substrate.
  • the resin flow resistance of the above-described first resin distribution medium is set at 1/10 or less of the resin flow resistance of the reinforcing fiber substrate or less, because the resin can be distributed into the medium quickly.
  • the distribution property of the resin injected into the first resin distribution medium in the surface direction of the reinforcing fiber substrate is ensured to be sufficiently high, the resin injected into the first resin distribution medium is quickly impregnated in the thickness direction of the reinforcing fiber substrate while the resin is distributed quickly in a direction along the surface.
  • the large/small relationship is given to the resin flow resistance of the first resin distribution medium and the resin flow resistance of the second resin distribution medium.
  • a peel ply capable of being removed together with a resin distribution medium after molding is interposed between at least one resin distribution medium and the reinforcing fiber substrate.
  • the resin distribution medium can be easily delaminated.
  • at least one resin distribution medium may be left in the molded product without delaminating it from the molded product. In this case, the peel ply is not necessary for the side where the resin distribution medium is left.
  • a method may be employed wherein a porous sheet is interposed between at least one resin distribution medium and the reinforcing fiber substrate.
  • This porous sheet has a function different from that of the above-described peel ply, and it is a sheet for suppressing a transfer of the irregularity of the resin distribution medium to the reinforcing fiber substrate side while maintaining the resin distribution function of the resin distribution medium. Therefore, the sheet is preferably disposed on the design surface side of the molded product.
  • At least one resin distribution medium may be formed by providing a groove as a resin flow path on an inner surface of the mold. In this case, even if a separate resin distribution medium is not made, it is possible to use the inner surface of the mold itself as a resin distribution medium.
  • a method can be employed wherein, in a case where at least two resin injection gates are disposed above the first resin distribution medium, the resin injection is carried out simultaneously from at least two resin injection gates adjacent to each other, or from all resin injection gates. Since the evacuation through the second resin distribution medium as well as the resin injection are carried out simultaneously while the quick resin impregnation is achieved, the generation of resin non-impregnation portions can be prevented.
  • a second method of RTM molding is characterized in that a reinforcing fiber substrate is placed in a mold, a resin distribution medium exhibiting a resin flow resistance lower than a resin flow resistance of the reinforcing fiber substrate is placed on a surface of the reinforcing fiber substrate opposite to the mold, a degasification medium comprising a gas permeation film and a gas permeable substrate is provided between the reinforcing fiber substrate and the mold, a resin is injected into the mold through the resin distribution medium after a pressure in the mold is reduced by evacuation, and the resin injected is impregnated into the reinforcing fiber substrate by evacuating the resin injected from a degasification space formed between the gas permeation film and the mold (a second method).
  • the above-described reinforcing fiber substrate comprises, for example, a laminate of reinforcing fiber materials.
  • the above-described gas permeation film has a releasability capable of being delaminated from a molded product after molding.
  • At least two resin injection gates are disposed above the resin distribution medium, and resin injection is carried out simultaneously from at least two resin injection gates adjacent to each other, or from all resin injection gates.
  • At least one evacuation route is provided in the mold in addition to an evacuation route from the degasific ation space formed between the gas permeation film and the mold.
  • the resin is injected into the first resin distribution medium having a lower resin flow resistance, and the injected resin is quickly impregnated into the reinforcing fiber substrate in the thickness direction while the resin is distributed quickly and broadly in a direction along the first surface of the reinforcing fiber substrate. Then, basically the inside of the mold is reduced in pressure by evacuation via the second resin distribution medium having a higher resin flow resistance, and the above-described injected resin is impregnated into the reinforcing fiber substrate having an evacuated and pressure-reduced condition.
  • the resin flow resistance (gas permeation resistance) of the second resin distribution medium is suppressed sufficiently low as compared with the resin flow resistance (gas permeation resistance) of the reinforcing fiber substrate although it is higher than the resin flow resistance (gas permeation resistance) of the first resin distribution medium, it is suppressed to reduce the vacuum degree in the substrate by deterioration of gas permeation from the reinforcing fiber substrate, and a quick resin impregnation can be ensured. Therefore, even for a thick reinforcing fiber substrate, a sufficiently good resin impregnation can be ensured.
  • the second resin distribution medium can be formed as a medium with a small irregularity as compared with the first resin distribution medium, and even if a transfer of the surface form of this second resin distribution medium to the surface of a molded product occurs, the degree of the irregularity on the surface of the molded product ascribed to the transfer can be suppressed small. Therefore, by setting this surface side to be a design surface side, a desirable design surface of the molded product having a small irregularity can be obtained.
  • the resin impregnation can be supplemented for a portion in which the resin is hardly impregnated into the reinforcing fiber substrate sufficiently, that is, for a portion of the second surface side, and it becomes possible to impregnate the resin sufficiently over the entire region of the reinforcing fiber substrate in the thickness direction.
  • the resin impregnation in the thickness direction of the reinforcing fiber substrate is carried out mainly by the impregnation from the first resin distribution medium side, and a lack of the impregnation is supplemented by the impregnation from the second resin distribution medium side.
  • the resin impregnation is supplemented, and voids pushed out from the first resin distribution medium side by the impregnated resin are pushed out at a relatively slow speed toward side portions, that is, in a direction along the second surface of the reinforcing fiber substrate, without being enclosed in the reinforcing fiber substrate by the resin impregnated from the second resin distribution medium side.
  • the aforementioned method of RTM molding (the second method) is effective for the following cases. namely, in a case where a flatness of a molded surface (a design surface) at the mold side is required further strongly, and in a molding where a resin impregnation into a thick and broad-area reinforcing fiber substrate is required, in particular, a degasification medium comprising a gas permeation film and a gas permeable substrate can be provided between the reinforcing fiber substrate and the surface of the mold as means for always effectively operating the degasification route from any portion of the mold surface.
  • the gas permeation film for example, preferably has fine holes on the surface and forms a flat surface. If such a film is employed, together with using a thin and small-irregularity substrate as the above-mentioned gas permeable substrate, the surface quality of a molded product can be improved.
  • the following method of RTM molding may be employed from the viewpoint of high Vf molding.
  • the method of RTM molding wherein a reinforcing fiber substrate is placed in a mold, a resin injection line and an evacuation line each communicating with an inside of the mold are provided, a pressure in the mold is reduced by evacuation and a resin is injected into the mold and impregnated into the reinforcing fiber substrate to form an FRP molded material, is characterized in that, after the resin is impregnated into the reinforcing fiber substrate so as to achieve a fiber volume content lower than a target fiber volume content of the FRP molded material, the injection of resin is stopped, and thereafter, evacuation of resin is continued until reaching the target fiber volume content (a third method).
  • a method can be employed wherein, after the injection of resin is stopped, at least one line of resin injection lines is changed to an evacuation line, and the evacuation of resin is continued until reaching the target fiber volume content.
  • the above-described target fiber volume content is preferably, for example, in a range of 55 to 65% to achieve a high Vf.
  • the above-described fiber volume content lower than the target fiber volume content is preferably, for example, in a range of 45 to 60%.
  • the resin impregnation property is required to be further increased, it is preferably in a range of 45 to 55%.
  • the above-described reinforcing fiber substrate can be formed as a preform having a fiber volume content, which is a rate of a volume of reinforcing fibers relative to a bulk volume of the reinforcing fiber substrate, lower than the target fiber volume content.
  • a woven fabric preformed at an arbitrary fiber volume content within a range lower than the target fiber volume content, or a laminate can be used as the reinforcing fiber substrate.
  • the laminate may be formed by laminating layers of reinforcing fibers by an arbitrary number, and a structure, where reinforcing fiber layers are bonded to each other, is more preferable because a stability is given to the fiber volume content.
  • the determination whether reaching the target fiber volume content or not can be carried out, for example, by measurement of the thickness of the reinforcing fiber substrate, and it may be determined whether an excessive resin is evacuated and removed by a predetermined amount or not by measuring this thickness during the continuation of the resin evacuation.
  • a method can be employed wherein an injection amount of resin corresponding to the fiber volume content lower than the target fiber volume content is preset, and the injection of resin is stopped at the time reaching the injection amount preset. Further, a method can be employed wherein an evacuation amount for reaching the target fiber volume content is preset relative to an injection amount of resin, and the evacuation of resin is stopped at the time reaching the evacuation amount preset.
  • At least one layer of the reinforcing fiber substrate comprises a carbon fiber layer, in order to obtain a high-strength and lightweight FRP molded material.
  • This carbon fiber layer can be formed as a woven fabric, for example, a unidirectional woven fabric in which carbon fibers are oriented unidirectionally.
  • the resin is impregnated into the reinforcing fiber substrate so that the fiber volume content becomes lower than the target fiber volume content of the FRP molded material, the porosity is high, the resin is impregnated sufficiently over the entire area of the reinforcing fiber substrate, and at that time, generation of resin non-impregnated portions can be prevented.
  • the resin injection is stopped, and thereafter, by the time when the resin is cured, the evacuation of resin is continued until reaching the target fiber volume content, and excessive resin is evacuated from the inside of the reinforcing fiber substrate, thereby achieving a target high Vf of the molded material.
  • the present invention provides a method of RTM molding as defined in the accompanying claims. Namely, in the method of RTM molding according to the present invention a plurality of reinforcing fiber materials are laminated in a mold to form a reinforcing fiber material laminate, and a resin is impregnated into the reinforcing fiber material laminate by injecting a resin in a direction from an end surface of the reinforcing fiber material laminate along a laminate surface while reducing a pressure in the mold by evacuation (a fourth method). Namely, the resin is injected from the end surface of the reinforcing fiber material laminate mainly into a portion between the reinforcing fiber materials, and the resin injected is impregnated into respective reinforcing fiber materials.
  • the resin is injected from the end surface of the reinforcing fiber material laminate in the direction along the laminate surface, first, the resin is injected quickly into a portion between the layers of the reinforcing fiber materials forming the reinforcing fiber material laminate, which is low in flow resistance, and thereafter, the resin is impregnated from the portion between the layers in the thickness direction of the respective reinforcing fiber materials, namely, in the lamination direction of the reinforcing fiber materials, and therefore, the matrix resin can be quickly injected and impregnated over the entire reinforcing fiber material laminate.
  • the limit in thickness such as a conventional limit does not exist, and the aforementioned problems can be solved at a time.
  • the resin flow resistance in the direction parallel to the surfaces of the reinforcing fiber materials is about 1/5-1/10 of the resin flow resistance in the direction perpendicular to the surfaces of the reinforcing fiber materials, according to experiment, although it is different depending on the kinds of the reinforcing fiber material and the resin, and the resin distribution speed in the direction parallel to the surfaces of the reinforcing fiber materials is very fast as compared with that in the perpendicular direction.
  • the molding condition is considered that the distance required for progressing the resin between the layers should be about 600 mm or less.
  • the restriction in thickness of the reinforcing fiber material laminate substantially does not exist, and the molding can be well carried out up to a thick molded material.
  • the irregularity of the resin distribution medium is not transferred, the surface property can be improved and a great cost down can be achieved by saving the processes for preparing and removing the resin distribution medium.
  • the gross length of the reinforcing fiber material laminate in a case where there is a bend or/and a curve, it is a total length along the shape
  • the resin injection from the above-described end surface into the portions between layers.
  • this length is more than 600 mm, the resin is hardly impregnated and there is a fear that a resin non-impregnated portion is generated.
  • the length is 300 mm or less, the resin impregnation becomes possible in a shorter time, and such a condition is more preferable.
  • the resin viscosity at a temperature for liquid resin injection is maintained in a range of 10 to 1500 mPa ⁇ s during a time from starting of the resin impregnation to expiration of one hour, a resin impregnation in a short period of time is possible.
  • the resin viscosity is less than 10 mPa ⁇ s, because the resin viscosity is too low, although the resin is quickly permeated in the portions between layers in the direction along the laminate surface, particularly in a case where the reinforcing fiber material is formed from a strand and the like, because the resin impregnation from the portion around the strand toward the inside of the strand progresses substantially simultaneously, a resin non-impregnated portion is liable to occur in the strand.
  • the resin viscosity at the temperature of liquid resin injection is maintained in a range of 10 to 1500 mPa ⁇ s during the time from starting of the resin impregnation to expiration of one hour.
  • the sectional shape of the reinforcing fiber material laminate is not particularly restricted, and it may be a rectangular, C-type, I-type, L-type, Z-type, T-type, J-type or hat shape, other than a flat plate shape.
  • the skin material is frequently formed in a simple flat plate shape but the stringer material is frequently formed in a relatively complicated shape, and in such a case, the present invention is suitably applied particularly to the part for forming the stringer material.
  • the present invention is suitable particularly for molding of this part for forming the stringer material. Namely, in the method, after the resin is injected from the end surface of the part for forming the stringer material of the laminate mainly into portions between layers of the respective reinforcing fiber materials, the resin injected is impregnated into the entire part for forming the stringer material.
  • these part for forming the stringer material and part for forming the skin material may be molded integrally Because the resin is injected from the end surface of the part for forming the stringer material, restriction in thickness of stringer material does not exist, and because it is not necessary to dispose a resin distribution medium, an improvement of surface property, and a great cost down due to saving of the preparing operation and the removing operation of the resin distribution medium, can be achieved.
  • a method can be employed wherein, for the part for forming the skin material, the resin is impregnated in the thickness direction while distributed in the direction along the surface of the part for forming the skin material via a resin distribution medium, and a reinforcing panel formed from the skin material and the stringer material is molded integrally.
  • a method can be employed wherein an upper mold provided with a resin distribution medium or a resin flow path groove is further disposed on the end surface of the reinforcing fiber material laminate.
  • Figures 9 to 11 illustrate molding apparatus for use in the presently claimed method of RTM molding.
  • Fig. 1 is a schematic vertical sectional view of a molding apparatus used for a method of RTM molding according to a first example.
  • a mold 1 forming a base is made, for example, from a stainless steel or an aluminum alloy, or another metal for mold or an FRP, and formed in, for example, a flat-plate like shape.
  • the shape of the mold 1 is processed depending on the shape of a desired molded product, and is not particularly restricted.
  • a breather 2 is disposed on mold 1 as a second resin distribution medium.
  • the "breather” has a resin flow resistance lower than a flow resistance of a resin flowing in a reinforcing fiber substrate although its resin flow resistance is not low as the flow resistance of the aforementioned conventional resin distribution medium.
  • the surface irregularity (surface roughness) of breather 2 is preferably 1.3 times or less of the surface irregularity (surface roughness) of the reinforcing fiber substrate.
  • a surface mat a plain weave woven fabric or a mesh woven fabric comprising glass fibers or carbon fibers which are reinforcing fibers and having a low weight (100 g/m 2 or less), or a woven fabric or a knit fabric comprising synthetic fibers and having a large denier (200 denier or more), is preferred.
  • a peel ply 3a is placed on breather 2. Peel ply 3a is laid in order to easily remove media and the like from a molded material, and as peel ply 3a, for example, a woven fabric having a releasing function such as a nylon taffeta is used.
  • reinforcing fiber substrate 4 is placed on peel ply 3a.
  • reinforcing fiber substrate 4 is formed as a laminate of a plurality of reinforcing fiber materials, in particular, a plurality of reinforcing fiber woven fabrics.
  • This apparatus is suitable particularly for the molding using such a thick reinforcing fiber substrate 4 laminated with a plurality of reinforcing fiber materials.
  • the apparatus can be applied, and also in such a case is suitable particularly for the molding using a thick reinforcing fiber substrate.
  • a first resin distribution medium 5 is placed on reinforcing fiber substrate 4 via peel ply 3b.
  • First resin distribution medium 5 has an irregularity on the surface, and in this example, the medium has a resin flow resistance of 1/10 or less of the resin flow resistance of reinforcing fiber substrate 4 (reinforcing fiber material laminate).
  • a large/small relationship in resin flow resistance is given between first resin distribution medium 5 and breather 2 as a second resin distribution medium, and the resin flow resistance of breather 2 is set higher than the resin flow resistance of first resin distribution medium 5.
  • first resin distribution medium 5 concretely, a mesh woven fabric made of polyethylene or polypropylene resin and having a mesh size of #400 or less is preferred.
  • first resin distribution medium 5 is disposed relative to the first surface of reinforcing fiber substrate 4, and breather 2 as the second resin distribution medium is disposed relative to the second surface at the opposite side.
  • bag material 8 comprises a gas-tight material for forming a pressure-reduced cavity, for this bag material 8, in consideration of thermal resistance, etc., for example, a nylon film is preferably used.
  • a resin injection gate 6c is provided relatively to first resin distribution medium 5 in the inside covered with bag material 8, and evacuation gates 6a, 6b for reducing the pressure of the inside by evacuation are provided relatively to breather 2 provided as the second resin distribution medium.
  • These gates 6a, 6b, 6c are formed, for example, by using C channel materials made of aluminum and the like, and these channel materials are connected to external members via plastic tubes.
  • a sealant 7 made of a synthetic rubber with a high adhesive property is interposed between the edge portion of bag material 8 and mold 1, and by sealing therebetween, flowing in of air from outside is prevented in order to maintain a pressure-reduced condition of the inside of bag material 8.
  • a thermosetting resin 10 prepared as an FRP matrix resin to be impregnated is stored in a resin pot 12 made of a plastic, and by opening a valve 9 at an appropriate timing, the resin is injected via resin injection gate 6c.
  • the inside of the cavity covered with bag material 8 is maintained at a pressure-reduced condition by a vacuum pump 11 via evacuation gates 6a, 6b.
  • bag material 8 is a double bag having a first bag material and a second bag material covering the first bag material, an air leakage can be prevented, and as a result, the fiber volume content (Vf) of reinforcing fibers can be increased.
  • bag material 8 is a single bag
  • the air leakage can be prevented by disposing sealant 7 at the outer edge portion as a parallel double disposition style, and an effect similar to that due to the double bag can be obtained.
  • the amount used for sub materials and the attachment time can be reduced rather than those in the double bag system, and there ir a merit capable of performing the molding more inexpensively.
  • ply 3b/resin distribution medium 5 are disposed on reinforcing fiber substrate 4 and peel ply 3a/breather 2 are disposed under the reinforcing fiber substrate 4 as in a conventional molding, it may be carried out that, after molding without disposing peel ply 3a, breather 2 is left in the molded material as it is.
  • the molding in this method is carried out as follows.
  • the laminate having a structure shown in Fig. 1 is placed on mold 1 (a tool), and the whole of the materials and members including resin injection gate 6c disposed at the upper side and evacuation gates 6a, 6b disposed at the lower side is covered with bag material 8.
  • bag material 8 In this state, when the resin is injected from resin injection gate 6c while the inside of bag material 8 is reduced in pressure by the evacuation through evacuation gates 6a, 6b, while matrix resin 10 is quickly distributed in first resin distribution medium 5 in a direction along the upper surface of reinforcing fiber substrate 4, the resin flows in a direction from the upper surface toward the lower surface and is impregnated into the reinforcing fiber substrate 4.
  • the resin is cured under a room temperature or a heated atmosphere, and thereafter, bag material 8 is delaminated and the molded material is released from the mold. Thereafter, peel plies 3a, 3b, resin distribution medium 5 and breather 2 are released and removed from the molded product.
  • breather 2 may be left in the molded product as it is.
  • first resin distribution medium 5 because the resin flow resistance of first resin distribution medium 5 is set low, the resin injected into the first resin distribution medium 5 is quickly impregnated into reinforcing fiber substrate 4 in the thickness direction while the resin is distributed in the direction along the first surface of the reinforcing fiber substrate 4 quickly and sufficiently broadly.
  • bag material 8 is evacuated via breather 2 provided as the second resin distribution medium in order to reduce the pressure in the bag material 8, because the resin flow resistance (gas permeation resistance) of breather 2 is suppressed sufficiently low as compared with the resin flow resistance (gas permeation resistance) of reinforcing fiber substrate 4 although it is higher than the resin flow resistance (gas permeation resistance) of first resin distribution medium 5, the reduction of vacuum degree in the substrate due to the deterioration of gas permeability from the reinforcing fiber substrate can be suppressed, and a quick resin impregnation property can be ensured. Therefore, even for a thick reinforcing fiber substrate 4, a sufficiently good resin impregnation property from the side of first resin distribution medium 5 can be ensured.
  • the breather 2 can be formed as a medium having a small irregularity as compared with the first resin distribution medium 5. Therefore, even if the surface pattern of such a breather 2 is transferred to the surface of a molded product, the degree of the irregularity of the surface of the molded product due to the transfer can be suppressed small. Namely, while a good resin impregnation property can be ensured, the irregularity of the surface of the molded product at the second resin distribution medium side can be suppressed small. By setting this surface side of the molded product having a small irregularity at a design surface side, a molded product having a desirable surface property can be obtained. Namely, it is possible to extinguish the traces of the medium which have been present in the tool surface side of the molded product by curing of the resin in the conventional method.
  • Fig. 2 is a schematic vertical sectional view of a molding apparatus according to a second example method, and Fig. 2 shows a case wherein, instead of the breather, a resin distribution medium 5a and a porous sheet 20 are disposed on one surface of the reinforcing fiber substrate.
  • Fig. 3 is a schematic vertical sectional view of a molding apparatus according to a third example, and Fig. 3 shows a case wherein, instead of the resin distribution medium disposed on the surface of the mold in Fig. 2 , the surface of the mold itself is formed as a resin distribution medium of the resin injection side by processing grooves on the mold.
  • the apparatus shown in Fig. 1 will be explained.
  • Symbol 20 indicates a porous sheet, and as the material of porous sheet 20, it is preferred to use a metal thin plate material (aluminum or stainless steel material), a steel punching metal with a thickness of 0.1 mm or more, a resin film with a thickness of 0.2 mm or more (a nylon, polyester, polyethylene, polypropylene or polyimide film), or an FRP sheet with a thickness of 0.2 mm or more.
  • a metal thin plate material aluminum or stainless steel material
  • a steel punching metal with a thickness of 0.1 mm or more
  • a resin film with a thickness of 0.2 mm or more a nylon, polyester, polyethylene, polypropylene or polyimide film
  • an FRP sheet with a thickness of 0.2 mm or more.
  • the hole is preferred to be circular-type from the viewpoint of processing, the shape is not particularly limited.
  • the hole diameter is preferably 3 mm or less, and more preferably 1.5 mm or less.
  • the arrangement of the holes may be either random or regular. Although a desirable pitch of the holes varies depending on the specification of the reinforcing fiber substrate to be used, it is preferably 15 mm or less, more preferably 10 mm or less.
  • the functions required for porous sheet 20 are as follows.
  • each groove 30 has a width of 0.5 mm to 5 mm and a depth of 1 mm to 6 mm and a pitch of the grooves is in a range of 2 mm to 25 mm, and the sectional shape is formed as a rectangular, reverse trapezoid or triangular shape. More preferably, the sectional shape of the groove is a rectangular shape having a width of about 1 mm and a depth of about 3 mm, and the pitch of the grooves is about 8 mm.
  • peel ply 3a/porous sheet 20/second resin distribution medium 5a are disposed in this order from the side contacting reinforcing fiber substrate 4 on the lower surface of the reinforcing fiber substrate 4.
  • the arrangement of porous sheet 20 and peel ply 3a may be reversed.
  • grooves for resin injection (example shown in the figure) or for evacuation may be provided on the tool surface (molding surface).
  • Fig. 4 is a schematic vertical sectional view of a molding apparatus according to a fourth example, and Fig. 4 shows a case wherein two evacuation gates 6d, 6e for reducing the pressure are provided on the reinforcing fiber substrate shown in Fig. 3 , and the resin is injected from both sides of the reinforcing fiber substrate by switching one gate 6d to a resin injection port on the way.
  • two evacuation gates 6d, 6e for reducing the pressure are provided on the reinforcing fiber substrate shown in Fig. 3 , and the resin is injected from both sides of the reinforcing fiber substrate by switching one gate 6d to a resin injection port on the way.
  • Evacuation gate 6d is switched to the resin injection port on the way of the molding.
  • valve 41 is opened, and when it is switched to a resin injection gate, after valve 41 is closed, valve 42 is opened.
  • reinforcing fiber substrate 4 is placed on the surface of the mold (tool) processed with grooves 30 via porous sheet 20 and peel ply 3a, and the whole of the materials and members including evacuation gates 6d, 6e disposed in plural on the upper surface side for reducing the pressure and the resin injection gate (grooves 30) disposed on the lower surface side is covered with the bag material.
  • valve 41 when valve 41 is opened, valve 42 and valve 9 are closed, while the inside of bag material 8 is evacuated and reduced in pressure by the evacuation through the evacuation gate, valve 9 is opened and the resin is injected into grooves 30 provided as the resin injection gate, matrix resin 10 flows and is impregnated from the lower surface to the upper surface of reinforcing fiber substrate 4.
  • the thickness of reinforcing fiber substrate 4 is 10 mm or more, depending on the combination of the resin and the reinforcing fiber substrate, there is a case that it is difficult to impregnate the resin completely up to the upper surface.
  • valve 41 can be closed and valve 42 can be opened, thereby switching at least one of the evacuation gates at the upper surface side (evacuation gate 6d in Fig. 4 ) to a resin injection gate.
  • the resin is injected also from the upper surface side, and the above-described lack of the resin impregnation can be supplemented.
  • the resin is flown from the side of gate 6d to the side of evacuation gate 6e, voids can be pushed out in the direction toward evacuation gate 6e accompanying with this resin flow.
  • porous sheet 20 having an appropriate stiffness interrupts the influence of the irregularity of the medium itself and a curing drop of the resin stored in the medium which occurs at the time of curing. Therefore, the surface property of the tool surface side of the molded product taken out after delaminating porous sheet 20/peel plies 3a, 3b/resin distribution medium 5 after releasing from the mold is exhibited as a surface property to which the flatness of the tool surface is almost reflected.
  • Fig. 5 is a schematic vertical sectional view of a molding apparatus used for a method of RTM molding according to a fifth example, and although the basic portions are the same as those in the aforementioned embodiments, it is different in that a degasification medium 54 comprising gas permeation film 50, gas permeable substrate 51 and seal tape 52 is provided on mold 1, and evacuation can be carried out from the degasification space formed between the gas permeation film 50 and the mold 1 through degasification port 53.
  • a degasification medium 54 comprising gas permeation film 50, gas permeable substrate 51 and seal tape 52 is provided on mold 1, and evacuation can be carried out from the degasification space formed between the gas permeation film 50 and the mold 1 through degasification port 53.
  • reinforcing fiber material laminate 4 is placed on the surface of mold 1 (tool), the whole of the materials and members including resin injection gate 6f disposed on the upper side and gas permeation film 50 and gas permeable substrate 51 disposed between mold 1 and laminate 4 is covered with bag material 8. In this case, all of the outer edge of gas permeation film 50 is sealed by a dhering it to the mold surface with seal tape 52.
  • gas permeation film 50 any material may be used as long as gas can be permeated but a resin and a liquid cannot be permeated, such as a fine porous sheet or resin film, or a substrate formed by coating a fine porous membrane onto a paper or fabric. Further, a film having a flatness on its surface can achieve a good surface quality of a molded product. Furthermore, although it is desirable that gas permeation film 50 has a releasing property, as the case may be, it is possible to integrate it with a molded product.
  • Gas permeable substrate 51 preferably has a good gas permeability in order to increase the impregnation property, and preferably has an irregularity as little as possible in order to improve the flatness of a molded product.
  • Fig. 6 shows a sixth example, and this example is an application example of the fifth example shown in Fig. 5 .
  • This method is a method for injecting a resin from at least two adjacent resin injection gates among a plurality of resin injection gates 6g, 6h, and the method is effective for a large molded product having a wide area.
  • laminate 5 is formed in a flat-plate like shape in Fig. 6 , even in a case of a molded product having a projection or a variation in thickness or a laminate difficult to control a resin flow such as a curved plate, it becomes possible to distribute a resin over the entire material.
  • evacuation gate 6a an evacuation route
  • evacuation gate 6a can be provided in addition to the above-described evacuation route from the degasification space, and this can be served to the control of impregnation direction at the time of resin injection or the evacuation of excessive resin after resin impregnation.
  • Fig. 7 shows an example of a molding apparatus used for a method of RTM molding according to a seventh example.
  • mold 1 forming a base is made, for example, from a stainless steel or an aluminum alloy, or another metal for mold or an FRP, and formed in, for example, a flat-plate like shape.
  • Reinforcing fiber substrate 4 is placed in this mold 1, in the figure, on mold 1.
  • Reinforcing fiber substrate 4 is formed, for example, as a laminate of a plurality of reinforcing fiber woven fabrics.
  • medium 5 for distributing a resin is placed on reinforcing fiber substrate 4 via peel ply 3.
  • Resin distribution medium 5 preferably has a resin flow resistance of 1/10 or less of the resin flow resistance in reinforcing fiber substrate 4, and concretely, a mesh woven fabric made of polyethylene or polypropylene resin and having a mesh size of #400 or less is preferred.
  • bag material 8 comprising a gas-tight material.
  • bag material 8 in consideration of gas-tight property and thermal resistance, for example, a nylon film is preferably used.
  • Sealant 7 made of a synthetic rubber with a high adhesive property prevents the flowing in of air from outside so that a pressure-reduced condition of the inside of bag material 8 can be maintained.
  • bag material 8 is formed as a double bag having a first bag material and a second bag material covering the first bag material, an air leakage can be prevented, and as a result, the Vf can be increased.
  • Resin injection port 6j and evacuation port 6i for reducing the pressure in bag material 8 by evacuation are provided in the sealed bag material 8, and the respective ports are connected to a resin injection line and an evacuation line.
  • resin injection port 6j and evacuation port 6i for example, aluminum C channel materials can be used, and these channel materials may be connected to external members vi plastic tubes forming the resin injection line and the evacuation line.
  • a thermosetting resin 10 prepared as a matrix resin for an FRP molded material is stored in a resin pot for example.
  • Vacuum trap 13 accumulates an excessive resin evacuated from the molded material through evacuation port 6i.
  • Vacuum pump 11 evacuates from the inside covered with bag material 8 through vacuum trap 13 and evacuation port 6i, and maintains a pressure-reduced condition in the inside. Peel ply 3 is interposed for easily removing resin distribution medium 5 from the molded material, and for it, for example, a woven fabric having a releasing function such as a nylon taffeta is used.
  • reinforcing fiber substrate 4 is not particularly restricted, for example, glass fibers, carbon fibers, aramide fibers, etc. can be raised. Further, a hybrid structure using or laminating two or more kinds of these fibers may be employed. Further, a sandwich structure interposing a core material such as a foam material or a hollow core between reinforcing fiber layers may be used. As reinforcing fiber substrate 4, it is preferred to use a woven fabric which is preformed at an arbitrary fiber content lower than a target fiber content or a laminate.
  • the woven fabric is preferably formed as a two-dimensional or three -dimensional structure
  • the laminate may be a laminate in which an arbitrary number of woven fabrics are laminated, and a preform in which woven fabrics are bonded to each other is more preferred from the viewpoint of stabilization of fiber content.
  • resin distribution medium 5 for example, a mesh-like material may be used, and a structure may be also employed wherein a resin flow path is formed on mold 1 by grooves and the like and the surface of the mold 1 formed with the resin flow path itself is formed as a resin distribution medium. Further, it is possible to use the reinforcing fiber substrate itself as a resin distribution medium.
  • the matrix resin for example, a polyester resin, a vinylester resin, an epoxy resin, a phenol resin, etc. can be raised.
  • Fig. 8 shows a molding apparatus used for a method of RTM molding according to an eighth example, and shows an apparatus wherein a substantial resin distribution medium is formed on the lower surface side of the reinforcing fiber substrate by processing grooves on the mold instead of disposing a resin distribution medium separately, and the thickness (thickness corresponding to the thickness of the molded material or the reinforcing fiber substrate impregnated with the resin) can be measured by a dial gauge during evacuation of resin. Point different from the apparatus shown in Fig. 7 are as follows.
  • Dial gauge 21 measures the thickness of the reinforcing fiber substrate during evacuation of resin.
  • Grooves 30 are processed on the mold for distributing the resin instead of a resin distribution medium, and it is preferred that each groove 30 has a width of 0.5 mm to 5 mm and a depth of 1 mm to 6 mm, the arrangement pitch of the grooves is in a range of 2 mm to 25 mm, and the cross-sectional shape of the groove is a reverse trapezoid, a triangle, etc More preferably, the width is about 1 mm, the depth is about 3 mm, the sectional shape is rectangular, and the pitch is about 8 mm.
  • a micrometer or laser measuring device can be raised.
  • reinforcing fiber substrate 4 is placed on the molding surface of mold 1, and thereon, peel ply 3 for releasing (for example, a nylon taffeta) and gas permeable material 23 (a polyester nonwoven fabric) are disposed.
  • peel ply 3 for releasing for example, a nylon taffeta
  • gas permeable material 23 a polyester nonwoven fabric
  • reinforcing fiber substrate 4 it is preferred to use a woven fabric which is preformed at an arbitrary fiber content lower than a target fiber volume content or a laminate. Because, when a resin is impregnated, it can be controlled at an arbitrary fiber content, and the impregnation is good and can be stabilized.
  • resin injection port 6j and evacuation port 6i are disposed, for example, at the end portion and the central portion ( Fig. 8 ) or at both end portions ( Fig. 7 ), and thereto a resin injection line and an evacuation line are connected, respectively.
  • resin injection port 6j are the resin injection line and evacuation port 6i and the evacuation line are provided at least one line, respectively.
  • bag material 8 is covered over the whole of the respective members laminated on mold 1 from the upper side, and the portion therearound is sealed by sealant 7 relatively to outside in order to maintain the inside of reinforcing fiber substrate 4, etc. at a pressure-reduced condition.
  • valves A1, A2 are closed, valve A3 is opened, and the inside is evacuated by vacuum pump 11 through evacuation port 6i, a vacuum line and vacuum trap 13, and the inside of the cavity (the inside covered with bag material 8) is reduced in pressure at 0.1 MPa or less.
  • mold 1 is placed in an oven for heating, and the whole of the mold is heated up to a predetermined temperature.
  • valve A1 is opened, and resin 10 is injected into the cavity through resin injection port 6j.
  • the resin is distributed in gas permeable material 23 toward the evacuation line, and the resin in the gas permeable material 23 is started to be impregnated into reinforcing fiber substrate 4.
  • valve A1 is closed and the supply of resin is stopped.
  • the fiber volume content Vf at the time of this stopping of resin injection is set in a range of 45% to 60%, more preferably, in a range of 50% to 55%. This is because of suppressing a resin loss due to evacuation as little as possible.
  • resin evacuation to resin trap 13 is carried out through evacuation port 6i communicated the vacuum line and resin injection port 6j after valve A2 is opened, until reaching the predetermined fiber volume content.
  • the resin evacuation may be continued until the resin becomes gel or the resin is cured, the evacuation is carried out until finally reaching the target fiber volume content of 55% to 65%.
  • To set the target fiber volume content in such a range is because, for example, in a case of members for air planes, it is necessary to set the Vf at 55% or more from the comparison in cost and performance with metal materials, and further, if the fiber volume content becomes a high Vf more than 65%, problems are liable to occur such as void generation by bad impregnation, reduction in shear strength between layers in the molded material, etc.
  • the target fiber volume content Vf can be set, for example, by the following method.
  • a method may be employed wherein a device for measuring the thickness of the laminate (reinforcing fiber substrate) ir disposed beforehand, and when the thickness reaches a thickness corresponding to the target fiber volume content while the thickness of the laminate is measured, valves A2 and A3 are closed.
  • the fiber volume content can be defined by the amounts of fibers and resin in the laminate
  • a method can be also employed wherein the amount of resin injection and the amount of evacuation corresponding to the predetermined fiber volume content is preset, the resin injection is stopped at the time reaching the target injection amount, and at the stage reaching the target evacuation amount, the resin evacuation is stopped.
  • the resin is cured at predetermined temperature and period of time.
  • all the submembers including the gas permeable material and members used for the resin injection and evacuation lines together with the bag material and the peel ply are removed, and finally, a molded product is released from the surface of the mold.
  • the molded material obtained is served to an aftercuring at predetermined temperature and period of time, as needed.
  • Fig. 9 shows an example of a molding apparatus used for a method of RTM molding according to an embodiment of the present invention.
  • mold 1 forming a base is made, for example, from a stainless steel or an aluminum alloy, or another metal for mold or an FRP, and formed in, for example, a flat-plate like shape.
  • a concave-type cavity is formed in mold 1.
  • Reinforcing fiber material laminate 4A is placed in this mold 1, in the figure, on mold 1.
  • Reinforcing fiber material laminate 4A is formed as a laminate of a plurality of reinforcing fiber materials 4, and each reinforcing fiber material 4 comprises, for example, a reinforcing fiber woven fabric.
  • Symbols 4a, 4b indicate the respective end surfaces of reinforcing fiber material laminate 4A formed in a thick flat plate-like shape.
  • resin distribution medium 5 for distributing a resin is disposed via peel ply 3.
  • peel ply 3 is disposed so as to cover the whole of reinforcing fiber material laminate 4A.
  • This resin distribution medium 5 has a low resin flow resistance of 1/10 or less of the resin flow resistance in reinforcing fiber material laminate 4A, and concretely, a mesh woven fabric made of polyethylene or polypropylene resin and having a mesh size of #400 or less is preferred.
  • bag material 8 comprising a gas-tight material.
  • bag material 8 in consideration of gas-tight property and thermal resistance, for example, a nylon film is preferably used.
  • Sealant 7 made of a synthetic rubber with a high adhesive property prevents the flowing in of air from outside so that a pressure-reduced condition of the inside of bag material 8 can be maintained.
  • peel ply 3 is laid in order to easily remove resin distribution medium 5 and the like from a molded material, and as peel ply 3, for example, a woven fabric having a releasing function such as a nylon taffeta can be used.
  • Resin injection port 6m and evacuation port 6k for reducing the pressure in bag material 8 by evacuation are provided in the sealed bag material 8, and the respective ports are connected to a resin injection line and an evacuation line.
  • resin injection port 6m and evacuation port 6k for example, aluminum C channel materials can be used, and these channel materials may be connected to external members via plastic tubes forming the resin injection line and the evacuation line.
  • a thermosetting resin 10 prepared as a matrix resin for an FRP molded material is stored in a plastic pot for example.
  • Vacuum trap 13 accumulates an excessive resin evacuated from the molded material through evacuation port 6k.
  • Vacuum pump 11 evacuates from the inside covered with bag material 8 through vacuum trap 13 and evacuation port 6k, and maintains a pressure-reduced condition in the inside.
  • Valves A1, B1 are provided for openin/closing the tubes of the resin injection line and the evacuation line, and for these, for example, joints with valves or pinch-off pliers can be used.
  • bag material 8 in a double-bag system having a first bag material and a second bag material covering the first bag material, an air leakage can be prevented, and as a result, the volume content of the reinforcing fibers (Vf) can be increased.
  • Fig. 10 shows a molding apparatus used for a method of RTM molding according to a second embodiment of the present invention, and shows an apparatus for molding a molded material with an integral composite formation comprising a stringer material with a composite shape, particularly, with an I-type cross section, and a flat plate-like skin material, as a fiber reinforced resin m olded material with a so-called skin/stringer integral structure.
  • Point different from the apparatus shown in Fig. 9 are as follows.
  • a laminate 4B (reinforcing fiber material laminate) of reinforcing fiber woven fabrics having a flat-plate like cross section forms a part for forming a skin material
  • a laminate 4C (reinforcing fiber material laminate) of reinforcing fiber woven fabrics having an I-type cross section forms a part for forming a stringer material.
  • Evacuation port 61 for reducing pressure and resin injection port 6n for injecting resin are provided, and C channel materials made of aluminum are preferably used for these ports. The channel materials are connected to external members via plastic tubes.
  • Jigs 14 are provided for fixing reinforcing fiber material laminate 4C forming the part for forming the stringer material at a C-type shape from both sides, respectively, and for the jigs 14, for example, metals or foamed cores can be used.
  • A5, A4 are valves for opening/closing the tubes, and for these valves, for example, joints with valves or pinch-off pliers can be used.
  • the injected resin flows in resin distribution medium 5 disposed over the exposed upper surface portion of part for forming the skin material 4B and the lower end surface portions of the reinforcing fiber material laminate of part for forming the stringer material 4C with an I-type cross section, and the resin is impregnated mainly in the thickness direction relatively to the part for forming the skin material 4B, and impregnated in the direction toward the portions between layers (a direction along the surface of the laminate of the reinforcing fiber materials) from the end surfaces of the reinforcing fiber material laminate relatively to the part for forming the stringer material 4C.
  • Fig. 11 shows a molding apparatus used for a method of RTM molding according to a third embodiment of the present invention, and shows an apparatus for molding a reinforcing fiber material laminate having a step.
  • 4D is a reinforcing fiber material laminate disposed partially on the upper surface of the laminate of reinforcing fiber materials 4 similar to those shown in Fig. 9 .
  • the injected resin flows in resin distribution medium 5 disposed so as to extend up to one end surface of reinforcing fiber material laminate 4D, and the resin is permeated in the lamination direction (thickness direction) relatively to the thin plate portion (a portion where the laminate 4D is not laminated), and impregnated in the direction parallel to the lamination direction (namely, the direction toward the portions between layers) from the end surface of the reinforcing fiber material laminate 4D via the resin distribution medium 5 disposed on the surface perpendicular to the lamination direction relatively to the thick plate portion (a portion where the laminate 4D is laminated).
  • a plurality of reinforcing fiber materials 4 are laminated on the molding surface of mold 1 to form reinforcing fiber material laminate 4A, and thereon, peel ply 3 for releasing (for example, nylon taffeta) is disposed so as to cover the whole of the laminate 4A.
  • peel ply 3 for releasing for example, nylon taffeta
  • the outer edge of peel ply 3 is disposed so as to reach up to sealant 7, as shown in Fig. 9 .
  • resin distribution medium 5 is disposed near both end portions of reinforcing fiber material laminate 4A so as to extend up to both end surfaces 4a, 4b of the laminate 4A, and further, thereon, resin injection port 6m and evacuation port 6k are disposed, respectively. Then, the whole of these materials is covered with bag material 8 (bag film), and the portion between the edge portion and mold 1 is sealed by sealant 7 over the entire circumference.
  • bag material 8 bag film
  • valve A1 is closed, and vacuum pump 11 is driven.
  • valve B1 is opened, and the inside of the cavity (the inside of bag material b) is evacuated from evacuation port 6k through vacuum trap 13.
  • the whole of the members on mold 1 is heated up to a predetermined molding temperature.
  • valve A4 is opened, matrix resin 10 is injected through resin injection port 6m by the reduced pressure in bag material 8. After the resin 10 is distributed through one resin distribution medium 5, first, the resin flows quickly in the portions between layers of reinforcing fiber material laminate 4A having a low flow resistance, and the resin reaches the opposite end portion of the laminate 4A.
  • the resin is impregnated in the thickness direction of the respective reinforcing fiber materials 4 from the respective portions between layers, namely in the lamination direction of reinforcing fiber materials 4, and at the time when the flow resistance reaches a balanced condition, the resin is impregnated uniformly over the entire area of the reinforcing fiber material laminate 4A.
  • the supply of the resin is stopped by closing valve A1. Thereafter, the resin is cured at predetermined temperature and period of time.
  • Examples 9 to 11 illustrate the method of claim 1; Reference Examples 1 to 8 are included for information only.
  • breather 2 glass fiber surface mat, weight: 80 g/m 2
  • evacuation gates 6a, 6b were disposed at both end portions, and vacuum pump was connected.
  • Peel ply 3a was disposed on breather 2, and thereon, reinforcing fiber substrate 4 comprising carbon fiber woven fabrics (produced by Toray Industries, Inc., plain weave fabric CO6343 using carbon fibers T300, weight: 200 g/m 2 ) laminated by 120 plies was disposed.
  • Peel ply 3b was disposed on reinforcing fiber substrate 4, thereon resin distribution medium 5 of a polypropylene mesh material (produced by Tokyo Polymer Corporation, "Netron"TSX-400P) was disposed, and thereon resin injection gate 6c was disposed and it was connected to resin pot 12 via valve 9.
  • the whole of these members was covered with bag material 8 (bag sheet), and the circumferential portion was sealed by sealant 7 (where, although omitted in the figure, a double-bag system was employed).
  • Valve 9 was closed, the inside of the cavity covered with bag material 8 was evacuated and reduced in pressure by vacuum pump 11, and the whole was heated at 60°C in an oven and the state was maintained for one hour.
  • thermosetting epoxy matrix resin 10 (the resin viscosity at 60°C (injection temperature): 200 mPa ⁇ s, the resin viscosity after expiration of one hour at 60°C: 300 mPa ⁇ s) was stored in resin pot 12 and valve 9 was opened, while the matrix resin 10 was distributed into the medium 5 through the resin injection line, the resin was impregnated in the thickness direction from the upper side toward the lower side, the substrate with a thickness of about 25 mm was completely impregnated with the resin without generating a non-impregnated portion.
  • valve 9 was closed to stop the supply of the resin, the whole was heated up to 130°C at about 2 °C/min., and the state was held for 2 hours, the matrix resin was cured. Thereafter, the temperature was lowered down to a room temperature at about 2°C/min., and the whole was taken out from the mold and the bag material 8 was removed. By delaminating the peel ply from the cured material, the cured resin on the surface of the molded product, the medium and the breather were removed. A surface good in surface flatness was obtained for the surface having contacted with the breather, although an irregularity was observed on the surface having contacted with the medium.
  • Porous sheet 20 (stainless steel punching metal with a thickness of 0.2 mm, in which holes each having a diameter of 1 mm were processed at a pitch of 10 mm) was disposed on the medium 5a, thereon peel ply 3a was disposed, and thereon, reinforcing fiber substrate 4 comprising carbon fiber woven fabrics (produced by Toray Industries, Inc., plain weave fabric CO6343 using carbon fibers T300, weight: 200 g/m 2 ) laminated by 120 plies was disposed.
  • carbon fiber woven fabrics produced by Toray Industries, Inc., plain weave fabric CO6343 using carbon fibers T300, weight: 200 g/m 2
  • Peel ply 3b was disposed on reinforcing fiber substrate 4, thereon medium 5b was disposed, and thereon resin injection port 6c was disposed and it was connected to resin pot 12 via valve 9 as a resin injection gate. At that time, a porous sheet may be disposed between peel ply 3b and medium 5b.
  • the whole of these members was covered with bag material 8 by a double bag system, and the circumferential portion was sealed by sealant 7.
  • Valve 9 was closed, the inside of the cavity covered with bag material 8 was reduced in pressure by vacuum pump 11, and the whole was heated at 60 °C in an oven and the state was maintained for one hour.
  • thermosetting epoxy matrix resin 10 (the resin viscosity at 60°C (injection temperature): 200 mPa ⁇ s, the resin viscosity after expiration of one hour at 60°C: 300 mPa ⁇ s) was stored in resin pot 12 and valve 9 was opened, while the matrix resin 10 was distributed into the upper medium 5b through the resin injection line, the resin was impregnated in the thickness direction of carbon fiber woven fabric laminate 4 from the upper side toward the lower side, the reinforcing fiber material laminate 4 with a thickness of about 25 mm was completely impregnated with the resin without generating a non-impregnated portion.
  • valve 9 was closed to stop the supply of the resin, the whole was heated up to 130°C at about 2°C/min., and the state was held for 2 hours, the matrix resin was cured, and thereafter, the temperature was lowered down to a room temperature at about 2°C/min., and the whole was taken out from the mold and the bag material 8 was removed.
  • the medium and the porous sheet a surface good in surface flatness was obtained for the surface having contacted with the porous sheet, although an irregularity was observed on the surface having contacted with the medium.
  • Porous sheet 20 (stainless steel punching metal with a thickness of 0.2 mm, in which holes each having a diameter of 1 mm were processed at a pitch of 10 mm) was disposed on the molding surface, thereon peel ply 3a was disposed, and thereon, reinforcing fiber substrate 4 comprising carbon fiber woven fabrics (produced by Toray Industries, Inc., plain weave fabric CO6343 using carbon fibers T300, weight: 200 g/m 2 ) laminated by 120 plies was disposed.
  • carbon fiber woven fabrics produced by Toray Industries, Inc., plain weave fabric CO6343 using carbon fibers T300, weight: 200 g/m 2
  • Peel ply 3b was disposed on reinforcing fiber substrate 4, thereon medium 5 of a polypropylene mesh material (produced by Tokyo Polymer Corporation, "Netron”TSX-400P) was disposed, and thereon, evacuation gate 6 was placed and it was connected to vacuum pump 11.
  • the whole of these members was covered with bag material 8 by a double bag system, and the circumferential portion was sealed by sealant 7.
  • Valve 9 was closed, the inside of the cavity covered with bag material 8 was reduced in pressure by vacuum pump 11, and the whole was heated at 60°C in an oven and the state was maintained for one hour.
  • thermosetting epoxy matrix resin 10 (the resin viscosity at 60°C (injection temperature): 200 mPa ⁇ s, the resin viscosity after expiration of one hour at 60°C: 300 mPa ⁇ s) was stored in resin pot 12 and valve 9 was opened, while the matrix resin 10 was distributed into the molding surface with grooves through the resin injection line, the resin was impregnated in the thickness direction of carbon fiber woven fabric laminate 4 from the lower side toward the upper side, the laminate 4 with a thickness of 25 mm was completely impregnated with the resin without generating a non-impregnated portion.
  • valve 9 was closed to stop the supply of the resin, the whole was heated up to 130°C at about 2°C/min., and the state was held for 2 hours, the matrix resin was cured, and thereafter, the temperature was lowered down to a room temperature at about 2°C/min., and the whole was taken out from the mold and the bag material 8 was removed.
  • Porous sheet 20 (stainless steel punching metal with a thickness of 0.2 mm, in which holes each having a diameter of 1 mm were processed at a pitch of 15 mm) was disposed on the molding surface, thereon peel ply 3a was disposed, and thereon, reinforcing fiber substrate 4 comprising carbon fiber woven fabrics (produced by Toray Industries, Inc., unidirectional woven fabric using carbon fibers T800S, weight: 190 g/m 2 ) laminated by 128 plies was disposed.
  • carbon fiber woven fabrics produced by Toray Industries, Inc., unidirectional woven fabric using carbon fibers T800S, weight: 190 g/m 2
  • Peel ply 3b was disposed on reinforcing fiber substrate 4, thereon medium 5 of a polypropylene mesh material (produced by Tokyo Polymer Corporation, "Netron”TSX-400P) was disposed, and thereon, evacuation gates 6d, 6e were placed and they were connected to vacuum pump 11.
  • the whole of these members was covered with bag material 8 by a double bag system, and the circumferential portion was sealed by sealant 7.
  • Valve 9 was closed, the inside of the cavity covered with bag material 8 was reduced in pressure by vacuum pump 11, and the whole was heated at 60°C in an oven and the state was maintained for one hour.
  • thermosetting epoxy matrix resin 10 (the resin viscosity at 60°C (injection temperature): 200 mPa ⁇ s, the resin viscosity after expiration of one hour at 60°C: 300 mPa ⁇ s) was stored in resin pot 12 and valve 9 was opened, while the matrix resin 10 was distributed into the molding surface with grooves through the resin injection line, the resin was impregnated in the thickness direction of carbon fiber woven fabric laminate 4 from the lower side toward the upper side. However, in a case where the state is held, at the time when the impregnation progresses up to a position of about 2/3 of the thickness of reinforcing fiber substrate 4, the resin impregnation becomes astringent.
  • valve 41 when the resin was impregnated up to a position of 1/2 of the thickness of reinforcing fiber substrate 4, valve 41 was stopped, valve 42 was opened, and evacuation gate 6d was switched to a resin injection gate.
  • the resin injected from gate 6d was distributed in distribution medium 5 in a direction toward evacuation gate 6e, and the resin was impregnated into the substrate in the downward direction via the inside of the medium 5. Finally, the resin was impregnated over the entire area of the inside of the substrate. Then, valve 9, 42 were closed to stop the supply of the resin.
  • the whole was heated up to 130°C at about 2°C/min., and the state was held for 2 hours, the matrix resin was cured, and thereafter, the temperature was lowered down to a room temperature at about 2°C/min., and the whole was taken out from the mold and the bag material 8 was removed.
  • reinforcing fiber substrate 4 (thickness: about 25 mm) comprising carbon fiber woven fabrics (produced by Toray Industries, Inc., plain weave fabric CO6343 using carbon fibers T300, weight: 200 g/m 2 ) laminated by 120 plies was disposed on gas permeation film 50.
  • peel ply 3b was disposed on reinforcing fiber substrate 4, thereon resin distribution medium 5 of a polypropylene mesh material (produced by Tokyo Polymer Corporation, "Netron”TSX-400P) was disposed, and thereon, resin injection gate 6f was placed and it was connected to resin pot 12 via valve 9.
  • the whole of these members was covered with bag material 8, and the circumferential portion was sealed by sealant 7 Valve 9 was closed, the inside of the cavity covered with bag material 8 was evacuated and reduced in pressure by vacuum pump 11, and the whole was heated at 70°C in an oven and the state was maintained for one hour.
  • thermosetting epoxy matrix resin 10 (the resin viscosity at 70°C (injection temperature): 130 mPa ⁇ s, the resin viscosity after expiration of one hour at 70°C: 320 mPa ⁇ s) was stored in the resin pot and valve 9 was opened, while the matrix resin 10 was distributed into the medium 5 through the resin injection line, the resin was impregnated in the thickness direction of reinforcing fiber substrate 4 from the upper side toward the lower side.
  • gas permeation film 50 does not exist, the gas present near the lower surface of the substrate is not well exhausted, the surface of the molded material obtained becomes "pockmarked-like", but, in this example, by providing gas permeation film 50, a degasification space was formed between the film and mold 1, the above-described gas was completely degasified from the entire area of the lower surface of reinforcing fiber substrate 4 through gas permeable substrate 51, and therefore, in spite of the thickness of the substrate of 25 mm, the resin was completely impregnated without any non-impregnated portion, and in particular, the surface quality was remarkably improved.
  • valve 9 was closed to stop the supply of the resin, the whole was heated up to 130°C at about 2°C/min., and the state was held for 2 hours, the matrix resin was cured. Thereafter, the temperature was lowered down to a room temperature at about 2°C/min., and the whole was taken out from the mold and the bag material 8 was removed. The lower surface of the cured molded product was obtained as a surface having a good surface flatness by delaminating gas permeation film 50.
  • reinforcing fiber substrate 4 (thickness: about 25 mm) comprising carbon fiber woven fabrics (produced by Toray Industries, Inc., plain weave fabric CO6343 using carbon fibers T300, weight: 200 g/m 2 ) laminated by 120 plies was disposed on gas permeation film 50.
  • evacuation gate 6a was disposed also on one side of the lower surface of the reinforcing fiber substrate.
  • Peel ply 3b was disposed on reinforcing fiber substrate 4, thereon resin distribution medium 5 of a polypropylene mesh material (produced by Tokyo Polymer Corporation, "Netron"TSX-400P) was disposed, and thereon, two resin injection gates 6g, 6h were placed and they were connected to resin pot 12 via valve 9. The whole of these members was covered with bag material 8, and the circumferential portion was sealed by sealant 7. Valve 9 was closed, the inside of the cavity covered with bag material 8 was evacuated and reduced in pressure by vacuum pump 11, and the whole was heated at 70°C in an oven and the state was maintained for one hour.
  • resin distribution medium 5 of a polypropylene mesh material (produced by Tokyo Polymer Corporation, "Netron"TSX-400P) was disposed, and thereon, two resin injection gates 6g, 6h were placed and they were connected to resin pot 12 via valve 9.
  • the whole of these members was covered with bag material 8, and the circumferential portion was sealed by sealant 7.
  • Valve 9 was closed, the inside of the cavity
  • thermosetting epoxy matrix resin 10 (the resin viscosity at 70 °C (injection temperature): 130 mPa ⁇ s, the resin viscosity after expiration of one hour at 70°C: 320 mPa ⁇ s) was stored in the resin pot and valve 9 was opened, while the matrix resin 10 flowed in medium 5 simultaneously through two resin injection lines and the resin was distributed on the surface, the resin was impregnated in the thickness direction of reinforcing fiber substrate 4 from the upper side toward the lower side, and the substrate with a thickness of about 25 mm was impregnated completely without any non-impregnated portion.
  • valve 9 was closed to stop the supply of the resin, the whole was heated up to 130°C at about 2°C/min., and the state was held for 2 hours, the matrix resin was cured.
  • the time for resin impregnation was short by the evacuation also through evacuation gate 6a, as compared with that in Example 5.
  • the temperature was lowered down to a room temperature at about 2 °C/min., and the whole was taken out from the mold and the bag material 8 was removed.
  • the lower surface of the cured molded product was obtained as a surface having a good surface flatness by delaminating gas permeation film 50.
  • a carbon fiber woven fabric cut at a length of 500 mm and a width of 500 mm was laid up on mold 1 comprising a stainless steel flat plate.
  • a reinforcing fiber material used for forming a reinforcing fiber substrate was a unidirectional woven fabric CZ8431DP (weight: 190 g/m 2 ) of "TORAYCA" T800S produced by Toray Industries, Inc., and it was laminated by 128 plies totally.
  • valves A1, A2 were closed, valve A3 was opened, and the evacuation was carried out through the evacuation port via the vacuum line and vacuum trap 13 to reduce the pressure in the cavity down to 0.1 MPa or less.
  • the mold was placed in an electric oven and the inside of the oven was heated at 60°C.
  • valve A1 was opened and matrix resin 10 was injected through resin injection port 6j at a vacuum pressure.
  • an epoxy resin (the resin viscosity at 60°C (injection temperature): 200 mPa ⁇ s, the resin viscosity after expiration of one hour at 60°C : 300 mPa ⁇ s) was used.
  • the injected resin was impregnated into the substrate 4 while flowing in resin distribution medium 5 having a low flow resistance.
  • valve A1 was closed to stop the supply of the resin.
  • the fiber volume content of the substrate capable of being estimated from the thickness of the reinforcing fiber substrate was about 48 %
  • valve A2 was opened, the resin injection line was opened to the vacuum side via the vacuum trap, and excessive resin in the reinforcing fiber substrate was evacuated into the vacuum trap 13 from the end portion of the reinforcing fiber substrate. Thereafter, at the time when the evacuation amount of the resin reached a predetermined amount of 1150 cm 3 , valves A2, A3 were closed to stop the supply of the resin. Then, the temperature in the electric oven was elevated up to 130°C, and heated and cured for about two hours. After the heat-curing, the sub members such as the bag material were removed, CFRP (carbon fiber reinforced plastic) molded material was released from the molding surface.
  • CFRP carbon fiber reinforced plastic
  • the fiber volume content of the CFRP molded material As the result of determination of the fiber volume content of the CFRP molded material at positions of the resin injection side, the evacuation side and an intermediate point therebetween, they were in a range of 57.2 % to 58.2 %. Namely, as compared with the time before resin evacuation immediately after resin impregnation, the fiber volume content could be increased up to a value within the range of the target value.
  • a carbon fiber woven fabric 4 cut at a length of 500 mm and a width of 500 mm was laid up on mold 1 comprising a stainless steel flat plate, on which #-type grooves 30 (width: 1 mm, depth: 4 mm, pitch: 15 mm) were processed as a flow path of resin.
  • the used carbon fiber woven fabric 4 was a unidirectional woven fabric CZ8431DP (weight: 190 g/m 2 ) of "TORAYCA" T800S produced by Toray Industries, Inc., and it was laminated by 128 plies totally.
  • gas permeable material 23 (polyester non-woven fabric) was disposed via peel ply 3, and thereon, evacuation port 6i was disposed.
  • resin injection port 6j was disposed on the grooves 30 for resin flow path formed on mold 1, the whole of these members was covered with bag material 8 (nylon film) by a double bag system and the circumferential portion was sealed by sealant 7 made of a synthetic rubber having a high adhesive property.
  • valves A1, A2 were closed, valve A3 was opened, and the evacuation was carried out through evacuation port 6i via the vacuum line and vacuum trap 13 to reduce the pressure in the cavity down to 0.1 MPa or less.
  • the mold was placed in an electric oven and the inside of the oven was heated at 60°C.
  • valve A1 was opened and matrix resin 10 was injected through resin injection port 6j at a vacuum pressure.
  • the resin the epoxy resin of Example 1 was used.
  • the injected resin was distributed in the grooves for distributing resin, and the resin in the grooves was impregnated into the substrate.
  • the fiber volume content was 48 %.
  • valve A1 was closed and valve A2 was opened, and excessive resin in the reinforcing fiber substrate was evacuated into vacuum trap 13.
  • the target fiber volume content of the CFRP molded material was set at 55 to 60 %. Since it was recognized from the experimental result beforehand that the curing shrinkage of the molded material in the thickness direction was about 1.2 %, at the time when the thickness became 23.8 mm, valves A2, A3 were closed to stop the evacuation of the resin. Thereafter, the temperature in the oven was elevated up to 130°C, and heated and cured for about two hours.
  • the present invention was applied to the molding of a thick flat plate.
  • a carbon fiber woven fabric 4 (reinforcing fiber material) cut at a length of 300 mm and a width of 300 mm was laid up on mold 1, comprising a stainless steel flat plate, by 128 plies, to form reinforcing fiber material laminate 4A having a total thickness of about 25 mm.
  • the used reinforcing fiber material was a unidirectional woven fabric CZ8431DP (weight: 190 g/m 2 ) of "TORAYCA" T800S produced by Toray Industries, Inc.
  • peel ply 3 nylon taffeta
  • resin distribution medium 5 polypropylene mesh material
  • resin injection port 6m and evacuation port 6k were disposed so as to communicate with both ends of the laminate 4A
  • bag material 8 nylon film
  • sealant 7 made of a synthetic rubber having a high adhesive property
  • valve A1 was closed, valve B1 was opened, and evacuation port 6k was communicated with the vacuum line via vacuum trap 13 communicated with the evacuation line, and the pressure in the cavity was reduced down to 0.1 MPa or less.
  • valve A1 was opened and matrix resin 10 was injected through resin injection port 6m under a pressure-reduced atmosphere with 0.08 to 0.1 MPa.
  • an epoxy resin the resin viscosity at 60°C. (injection temperature): 200 mPa ⁇ s, the resin viscosity after expiration of one hour at 60°C : 300 mPa ⁇ s was used.
  • the injected resin first flowed in resin distribution medium 5 having a low flow resistance, and at the time reaching the end of reinforcing fiber material laminate 4A, the resin flowed therefrom mainly in the laminate 4A in the direction along the lamination surface of the laminate 4A, and thereafter, the resin was impregnated in the thickness direction, and this resin flow was observed from the above position of transparent bag material 8.
  • valve A1 was closed to stop the supply of the resin. Thereafter, the temperature in the oven was elevated up to 130°C, and heated and cured for about two hours. After the heat-curing, the sub members such as the bag material 8 were removed, and the CFRP molded material was taken out from the molding surface. As a result, the CFRP molded material was completely impregnated with resin in spite of a relatively small thickness of 25 mm. Further, the surface property of the molded material was flat.
  • the present invention was applied to the molding of a skin/stringer integrally structural material.
  • a carbon fiber woven fabric 4 (reinforcing fiber material) cut at a length of 500 mm and a width of 500 mm was laid up on mold 1 to form reinforcing fiber material laminate 4B.
  • the used reinforcing fiber material was a unidirectional woven fabric (weight: 190 g/m 2 ) of "TORAYCA” T800S produced by Toray Industries, Inc., and it was laminated by 128 plies totally (hereinafter, referred to as "reinforcing fiber material laminate for forming a skin material 4B").
  • a carbon fiber woven fabric 4 cut at a width of 98 mm and a length of 500 mm was placed by 32 plies using jig 14 for fixing a C-type shape.
  • Another laminate of the carbon fiber woven fabric 4 was further prepared, and the two laminates were disposed so as to form a structure back to back symmetrically with jigs 14 disposed at both sides to form a reinforcing fiber material laminate having an I-type cross section, and it was placed on the reinforcing fiber material laminate for forming a skin material 4B which had been already 1 aid up.
  • reinforcing fiber material laminate placed on the reinforcing fiber material laminate for forming a skin material 4B is referred to as "reinforcing fiber material laminate for forming a stringer material 4C").
  • peel ply 3 nylon taffeta
  • resin distribution medium 5 polypropylene mesh material
  • resin injection ports 6m, 6n and evacuation ports 6k, 6l were disposed on these reinforcing fiber material laminates, as shown in Fig. 10 .
  • bag material 8 nylon film
  • sealant 7 made of a synthetic rubber having a high adhesive property.
  • valves A4, A5 were closed, valves B1, B2 were opened, and evacuation ports 6k, 6l were opened via vacuum trap 13 communicated with the vacuum line, and the pressure in the cavity was reduced down to 0.1 MPa or less.
  • the mold was placed in an electric oven and the inside of the oven was heated at 70°C.
  • valves A4, A5 were opened and matrix resin 10 was injected through resin injection ports 6m, 6n under a pressure-reduced condition.
  • an epoxy resin the resin viscosity at 70°C (injection temperature): 130 mPa ⁇ s, the resin viscosity after expiration of one hour at 60°C : 320 mPa ⁇ s
  • the injected resin flowed in the resin distribution medium having a low flow resistance, and was impregnated into the substrate.
  • the resin was impregnated in the thickness direction relatively to the reinforcing fiber material laminate for forming a skin material 4B, relatively to the reinforcing fiber material laminate for forming a stringer material 4C, the resin flowed in the direction of portions between layers of the laminate from the end surface of the lower side of the I-type reinforcing fiber material laminate, and was impregnated mainly in the thickness direction of the respective reinforcing fiber materials (namely, the thickness direction of the 1-type reinforcing fiber material laminate) after being permeated into the I-type reinforcing fiber material laminate.
  • valves A4, A5 were closed to stop the supply of the resin.
  • the temperature in the oven was elevated up to 130°C, and heated and cured for about two hours.
  • the sub members such as the bag material 8 were removed, and the CFRP molded material was taken out from the molding surface.
  • the CFRP molded material obtained the resin was completely impregnated particularly up to the corners of the stringer part. Further, the surface property of the stringer part was flat.
  • the present invention was applied to the molding of a panel with a step.
  • a carbon fiber woven fabric 4 (produced by Toray Industries, Inc., plain weave fabric CO6343 using carbon fibers T300, weight: 190 g/m 2 ) cut at a length of 500 mm and a width of 500 mm was laid up by 24 plies on mold 1 of an aluminum flat plate, and thereon, the carbon fiber woven fabric cut at a length of 150 mm and a width of 500 mm was laid up by 56 plies was laid up as a thick plate portion, to form reinforcing fiber material laminate 4D.
  • Fig. 11 a carbon fiber woven fabric 4 (produced by Toray Industries, Inc., plain weave fabric CO6343 using carbon fibers T300, weight: 190 g/m 2 ) cut at a length of 500 mm and a width of 500 mm was laid up by 24 plies on mold 1 of an aluminum flat plate, and thereon, the carbon fiber woven fabric cut at a length of 150 mm and a width
  • valves A1, A2 were closed to stop the resin injection, the electric oven was heated up to 130°C, and the resin was cured for about two hours at a condition keeping the temperature.
  • the sub members such as the bag material 8 were removed, and the CFRP molded material was taken out from the molding surface.
  • the resin was completely impregnated particularly as to all portions of the thin plate portion and the thick plate portion, and the surface property of the stringer part was flat.
  • the method of RTM molding according to the present invention is suitable particularly for molding of a thick FRP structural material, and according to the present invention, an FRP structural material, having an excellent designability, or having excellent lightweight property and strength by increase of fiber volume content, can be molded.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)

Claims (8)

  1. Procédé de moulage RTM dans lequel une pluralité de matériaux à fibres de renforcement (4) sont stratifiés dans un moule (1) pour former un stratifié de matériau à fibres de renforcement (4A) ayant des surfaces d'extrémité (4a, 4b), dans lequel un milieu de distribution de résine (5) pour distribuer de la résine par rapport aux surfaces d'extrémité (4a, 4b) du stratifié de matériau à fibres de renforcement (4A) est disposé par le biais d'une couche pelable (3) qui recouvre l'ensemble du stratifié à fibres de renforcement (4A), dans lequel le milieu de distribution de résine a une faible résistance à l'écoulement inférieure ou égale à 1/10 de la résistance à l'écoulement de la résine dans le stratifié de matériau à fibres de renforcement (4A), l'ensemble des matériaux disposés sur le moule (1) sont recouverts avec un matériau d'ensachage (8) comprenant un matériau étanche aux gaz et scellé avec un agent d'étanchéité (7) ayant une propriété d'adhérence élevée pour empêcher l'écoulement d'air depuis l'extérieur, un orifice d'injection (6m) et un orifice d'évacuation (6k) de résine sont prévus dans le matériau d'ensachage (8) et sont raccordés respectivement à une ligne d'injection de résine et une ligne d'évacuation de résine, chacun d'eux possédant un robinet (A1, B1) pour ouvrir et fermer la ligne, une résine thermodurcissable est fournie en tant que résine matricielle, et une pompe à vide (11) est agencée pour assurer l'évacuation depuis l'intérieur, recouverte avec le matériau d'ensachage (8) à travers l'orifice d'évacuation (6k) et un piège à vide (13) ; procédé dans lequel une résine matricielle est imprégnée dans le stratifié de matériau à fibres de renforcement (4A) en injectant la résine dans une direction partant de la surface d'extrémité (4a) du stratifié de matériau à fibres de renforcement (4A) le long d'une surface de stratifié et entre les couches de matériaux à fibres (4) tout en réduisant une pression dans le moule (1) par évacuation.
  2. Procédé de moulage RTM selon la revendication 1, dans lequel une longueur brute dudit stratifié de matériau à fibres de renforcement est inférieure ou égale à 600 mm.
  3. Procédé de moulage RTM selon la revendication 1 ou 2, dans lequel une viscosité de résine à une température d'injection de résine est maintenue dans une plage de 10 à 1500 mPa·s au cours d'une période allant du début de l'imprégnation de résine à l'expiration d'un délai d'une heure.
  4. Procédé de moulage RTM selon l'une quelconque des revendications 1 à 3, dans lequel une forme en coupe dudit stratifié de matériau à fibres de renforcement est une forme rectangulaire, de type en C, de type en 1, de type en L, de type en Z, de type en T, de type en J ou en chapeau.
  5. Procédé de moulage RTM selon l'une quelconque des revendications 1 à 4, dans lequel ledit stratifié de matériau à fibres de renforcement comprend une partie conçue pour former un matériau de lisse ayant une section de forme rectangulaire, de type en C, de type en I, de type en L, de type en Z, de type en T, de type en J ou en chapeau, et une partie conçue pour former un matériau de revêtement.
  6. Procédé de moulage RTM selon la revendication 5, dans lequel, après que ladite résine est injectée depuis une surface d'extrémité de ladite partie conçue pour former un matériau de lisse dudit stratifié principalement dans une partie entre les couches desdits matériaux à fibres de renforcement, la résine injectée est imprégnée dans la totalité de la partie conçue pour former un matériau de lisse.
  7. Procédé de moulage RTM selon la revendication 6, dans lequel pour ladite partie conçue pour former un matériau de revêtement, ladite résine est imprégnée dans le sens de l'épaisseur tout en étant distribuée dans une direction le long d'une surface de ladite partie conçue pour former un matériau de revêtement par le biais d'un milieu de distribution de résine, et un panneau de renforcement formé à partir dudit matériau de revêtement et dudit matériau de lisse est moulé d'un seul tenant.
  8. Procédé de moulage RTM selon l'une quelconque des revendications 1 à 6, dans lequel un moule supérieur doté d'un milieu de distribution de résine ou d'une rainure de trajet d'écoulement de résine est en outre disposé sur ladite surface d'extrémité dudit stratifié de matériau à fibres de renforcement.
EP13173654.8A 2002-10-09 2003-10-09 Méthode de moulage RTM Expired - Lifetime EP2644365B1 (fr)

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
JP2002295933A JP4104413B2 (ja) 2002-10-09 2002-10-09 Ｒｔｍ成形方法
JP2002295932 2002-10-09
JP2002295934A JP4104414B2 (ja) 2002-10-09 2002-10-09 繊維強化樹脂成形体の製造方法
JP2002312454A JP4104422B2 (ja) 2002-10-09 2002-10-28 Ｒｔｍ成形方法
PCT/JP2003/012947 WO2004033176A1 (fr) 2002-10-09 2003-10-09 Procede de moulage rtm
EP03751403.1A EP1555104B1 (fr) 2002-10-09 2003-10-09 Procede de moulage de pastique renforce de fibres

Related Parent Applications (3)

Application Number Title Priority Date Filing Date
EP03751403.1 Division 2003-10-09
EP03751403.1A Division-Into EP1555104B1 (fr) 2002-10-09 2003-10-09 Procede de moulage de pastique renforce de fibres
EP03751403.1A Division EP1555104B1 (fr) 2002-10-09 2003-10-09 Procede de moulage de pastique renforce de fibres

Publications (3)

Publication Number Publication Date
EP2644365A2 EP2644365A2 (fr) 2013-10-02
EP2644365A3 EP2644365A3 (fr) 2014-08-13
EP2644365B1 true EP2644365B1 (fr) 2019-03-27

Family

ID=32097011

Family Applications (4)

Application Number Title Priority Date Filing Date
EP13173654.8A Expired - Lifetime EP2644365B1 (fr) 2002-10-09 2003-10-09 Méthode de moulage RTM
EP13173648.0A Expired - Fee Related EP2644363B1 (fr) 2002-10-09 2003-10-09 Méthode de moulage RTM
EP03751403.1A Expired - Fee Related EP1555104B1 (fr) 2002-10-09 2003-10-09 Procede de moulage de pastique renforce de fibres
EP20130173653 Withdrawn EP2644364A3 (fr) 2002-10-09 2003-10-09 Méthode de moulage RTM

Family Applications After (3)

Application Number Title Priority Date Filing Date
EP13173648.0A Expired - Fee Related EP2644363B1 (fr) 2002-10-09 2003-10-09 Méthode de moulage RTM
EP03751403.1A Expired - Fee Related EP1555104B1 (fr) 2002-10-09 2003-10-09 Procede de moulage de pastique renforce de fibres
EP20130173653 Withdrawn EP2644364A3 (fr) 2002-10-09 2003-10-09 Méthode de moulage RTM

Country Status (5)

Country Link
US (4) US8420002B2 (fr)
EP (4) EP2644365B1 (fr)
AU (4) AU2003271139B2 (fr)
ES (2) ES2628600T3 (fr)
WO (1) WO2004033176A1 (fr)

Families Citing this family (70)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0417634D0 (en) * 2004-08-09 2004-09-08 Structural Polymer Systems Ltd Mould
DK176150B1 (da) 2004-11-30 2006-10-16 Lm Glasfiber As Fremgangsmåde og apparat til fremstilling af fiberkompositemner ved vakuuminfusion
DK176135B1 (da) 2004-11-30 2006-09-18 Lm Glasfiber As Vakuuminfusion ved hjælp af semipermeabel membran
US20060134408A1 (en) * 2004-12-20 2006-06-22 Mitsubishi Rayon Co., Ltd. Process for producing sandwich structure and adhesive film therefor
US7842209B2 (en) * 2006-02-21 2010-11-30 The Boeing Company Vacuum debulk and radiation cure method
US20080186691A1 (en) * 2006-04-28 2008-08-07 Mertz John C Implantable medical device housing reinforcement
JP4444248B2 (ja) * 2006-08-08 2010-03-31 三菱重工業株式会社 Ｒｔｍ成形装置及びｒｔｍ成形体の製造方法
DE102007013987A1 (de) * 2006-08-17 2008-02-21 Airbus Deutschland Gmbh Werkzeug zur Herstellung von Faserverbundbauteilen
US20080136060A1 (en) * 2006-12-08 2008-06-12 Gkn Westland Aerospace, Inc. System and method for forming and curing a composite structure
WO2008114809A1 (fr) * 2007-03-20 2008-09-25 Mitsubishi Heavy Industries, Ltd. Procédé de rtm assisté sous vide
FR2920336B1 (fr) * 2007-09-05 2012-09-28 Eads Europ Aeronautic Defence Methode et dispositif d'analyse des procedes de fabrication de pieces en materiaux composites, par infusion ou injection, et de caracterisation de ces materiaux composites.
FR2926241B1 (fr) * 2008-01-16 2013-03-15 Eads Europ Aeronautic Defence Procede et dispositif de moulage d'une piece en materiau composite
CA2739517C (fr) * 2008-11-18 2013-08-27 Mitsubishi Heavy Industries, Ltd. Equipement pour la fabrication d'un materiau composite et procede de fabrication d'un materiau composite
DE102009021591B4 (de) * 2009-05-15 2012-12-20 Eads Deutschland Gmbh Verfahren zum Preformen eines Textilienhalbzeugs und Preform-Vorrichtung
FR2948600B1 (fr) 2009-07-28 2011-10-07 Airbus Operations Sas Procede de fabrication d'une piece d'aeronef par infusion de resine
EP2295235B1 (fr) * 2009-08-20 2013-07-03 Siemens Aktiengesellschaft Structure plastique renforcée à fibre et procédé pour produire la structure plastique renforcée à fibre
US8940213B2 (en) 2010-06-25 2015-01-27 The Boeing Company Resin infusion of composite parts using a perforated caul sheet
US9682514B2 (en) 2010-06-25 2017-06-20 The Boeing Company Method of manufacturing resin infused composite parts using a perforated caul sheet
JP5533743B2 (ja) * 2010-09-24 2014-06-25 東レ株式会社 繊維強化プラスチックの製造方法
WO2012082778A2 (fr) * 2010-12-17 2012-06-21 3M Innovative Properties Company Article composite et son procédé de fabrication
US9604415B2 (en) * 2011-02-25 2017-03-28 Toray Industries, Inc. Method for producing FRP
JP5693296B2 (ja) * 2011-02-28 2015-04-01 三菱重工業株式会社 Ｒｔｍ成形装置及びｒｔｍ成形方法、並びに半成形体
DE102011016368A1 (de) * 2011-04-07 2012-10-11 Deutsches Zentrum für Luft- und Raumfahrt e.V. Herstellung von faserverstärkten Kunststoffen
DK2561977T3 (da) * 2011-08-24 2014-08-11 Nordex Energy Gmbh Fremgangsmåde til fremstilling af en vindenergianlæg-rotorbladsdel med et kulfiberforstærket hovedbånd
FR2979574B1 (fr) * 2011-09-07 2016-12-09 Airbus Operations Sas Procede de fabrication d'une structure comprenant une peau et des raidisseurs
EP2750866B1 (fr) * 2011-11-17 2017-08-16 Siemens Aktiengesellschaft Système et méthode d'envoi d'un fluide dans un moule pour le moulage d'une structure composite renforcée
JP5646089B2 (ja) * 2011-12-06 2014-12-24 三菱電機株式会社 プリフォームの製造方法および繊維強化プラスチック成形体の製造方法
RU2601455C2 (ru) * 2011-12-13 2016-11-10 Стевик Сас Многослойный листовой материал для вакуумного формования
RU2480335C1 (ru) * 2012-02-07 2013-04-27 Закрытое Акционерное Общество "Аэрокомпозит" Способ изготовления волокнистых композитов вакуумной инфузией и устройство для осуществления способа
RU2480334C1 (ru) * 2012-02-07 2013-04-27 Закрытое Акционерное Общество "Аэрокомпозит" Способ изготовления изделий из волокнистого полимерного композиционного материала поверхностным инфузионным процессом и устройство для осуществления способа
RU2496640C1 (ru) * 2012-03-22 2013-10-27 Открытое акционерное общество "Национальный институт авиационных технологий" (ОАО НИАТ) Способ изготовления изделия из полимерного композиционного материала трансферно-мембранным формованием "тмф" (варианты)
US9199419B2 (en) * 2012-10-31 2015-12-01 The Boeing Company System and method for facilitating fluid movement in close-molded composite parts
DE102013108568B4 (de) * 2013-01-08 2016-08-04 Deutsches Zentrum für Luft- und Raumfahrt e.V. Ermittlung der Bauteildicke eines Faserverbundbauteils
BR112015020629A2 (pt) * 2013-02-26 2017-07-18 Hexcel Holding Gmbh fabricação de uma peça moldada
US20140265058A1 (en) * 2013-03-13 2014-09-18 North Thin Ply Technology Llc System and method for maneuvering thin ply technology complexes
DE102013205685A1 (de) * 2013-03-28 2014-10-16 Universität Stuttgart Verfahren und Vorrichtung zum Imprägnieren von Faserhalbzeugen
EP2799215B1 (fr) * 2013-05-02 2018-09-19 Siemens Aktiengesellschaft Membrane à vide perforée pour stratifiés renforcés par des fibres
JP6154670B2 (ja) * 2013-06-06 2017-06-28 三菱航空機株式会社 繊維強化プラスチック部材の成形方法及び成形装置
DE102013012762B4 (de) * 2013-07-31 2017-05-04 Mt Aerospace Ag Verfahren zur Herstellung von Faserverbundgehäusen mit integrierter Isolation
GB2519160B (en) * 2013-10-11 2016-06-22 Spirit Aerosys Inc Method of liquid resin infusion of a composite preform
CN104576411A (zh) * 2013-10-25 2015-04-29 飞思卡尔半导体公司 双角部顶部闸道模制
US9403350B2 (en) * 2013-12-16 2016-08-02 The Nordam Group, Inc. Flash control metal bonding
US10961360B2 (en) 2014-01-10 2021-03-30 Komatsu Matere Co., Ltd. Fiber-reinforced resin material and molded fiber-reinforced resin body obtained using the same
JP6116497B2 (ja) * 2014-02-27 2017-04-19 三菱重工業株式会社 樹脂流動制御システムおよび樹脂流動制御方法
DE102014007869B4 (de) 2014-06-03 2016-02-11 Airbus Defence and Space GmbH Vorrichtung und Verfahren zum Infiltrieren von Fasermaterial mit Harz zur Herstellung eines Faserverbundbauteils
EP3175979B1 (fr) * 2014-07-31 2020-03-04 KOMATSU MATERE Co., Ltd. Objet moulé et procédé de production associé
MX2017005201A (es) * 2014-10-30 2018-09-18 Lm Wp Patent Holding As Fabricación de banda de cizalla en forma de i.
WO2016090405A1 (fr) * 2014-12-08 2016-06-16 Peter John Murdoch Procédé de formation d'un composant composite métallique à fibres
CN106142593B (zh) 2015-04-10 2019-11-26 科思创德国股份有限公司 制造纤维增强塑料制品的方法
JP2016221733A (ja) * 2015-05-28 2016-12-28 三菱航空機株式会社 ＶａＲＴＭ工法による成形方法
US9951641B2 (en) * 2015-07-14 2018-04-24 CTL Aerospace, Inc. Resin transfer molding process
CA2942015C (fr) * 2015-09-14 2019-01-15 Bell Helicopter Textron Inc. Methode de formation d'un coussin de pression ou autre element souple servant pendant le durcissement de materiau composite
DE102015120572A1 (de) * 2015-11-26 2017-06-01 Airbus Operations Gmbh Harzsperrvorrichtung für ein Infusionswerkzeug
US10357922B2 (en) * 2016-01-07 2019-07-23 The Boeing Company Edge breathers for composite products
KR101936584B1 (ko) 2016-02-03 2019-01-09 (주)엘지하우시스 프리프레그 제조 장치 및 이를 이용한 프리프레그 제조 방법
US10384399B2 (en) 2016-03-08 2019-08-20 The Boeing Company Systems and methods for depositing compounds in a structure
US10512857B2 (en) 2016-03-08 2019-12-24 The Boeing Company Systems and methods for viscous material vacuum deaeration, and systems and methods for depositing compounds in a structure
JP6591661B2 (ja) * 2016-04-07 2019-10-16 三菱重工業株式会社 複合材の製造方法
US9944063B1 (en) * 2016-05-23 2018-04-17 Boral Ip Holdings (Australia) Pty Limited Method of producing reinforced substrate
WO2018030470A1 (fr) * 2016-08-09 2018-02-15 三菱重工業株式会社 Procédé de production d'articles moulés en résine renforcée de fibres
EP3299154A1 (fr) * 2016-09-27 2018-03-28 Hexcel Reinforcements SAS Dispositif de production d'une partie composite
MX2019007759A (es) * 2016-12-27 2019-08-22 Continental Structural Plastics Inc Moldeo por transferencia de resina de canal continuo con tiempo de ciclo rápido.
US11097524B2 (en) * 2017-05-26 2021-08-24 The Boeing Company Flexible vacuum securement of objects to complex surfaces
GB2570104B (en) * 2017-12-18 2021-12-29 Composite Integration Ltd Improved system and method for resin transfer moulding
CN107984562B (zh) * 2017-12-31 2023-11-28 浙江省林业科学研究院 一种rtm成型竹束复合板材制造方法
JP7114266B2 (ja) * 2018-02-13 2022-08-08 三菱重工業株式会社 複合材料の製造方法および繊維基材
CN111284038A (zh) * 2018-12-07 2020-06-16 中航贵州飞机有限责任公司 一种无人机用带筋复合材料件的液态成型方法
EP3712423B1 (fr) * 2019-03-21 2022-12-28 Siemens Gamesa Renewable Energy A/S Procédé de réparation d'un capuchon de longeron endommagé d'une pale d'éolienne d'une éolienne
DE102021208517B4 (de) 2021-08-05 2024-05-02 Innfa Gmbh Verfahren, Verwendung einer Anlage und Spule zum Behandeln, insbesondere Imprägnieren, von Endlosfasern
CN113954389A (zh) * 2021-09-30 2022-01-21 湖北三江航天江北机械工程有限公司 高强度高纤维体积含量树脂基复合材料的制备方法及设备

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2913036A (en) * 1956-08-10 1959-11-17 Anthony Bros Fibre Glass Pool Process and apparatus for molding large plastic structures
US3975479A (en) * 1973-03-09 1976-08-17 Mcclean Anderson, Inc. Method of fabricating a reinforced plastic article
JPS56127426A (en) 1980-03-11 1981-10-06 Hitachi Chem Co Ltd Manufacture of fiber-reinforced thermosetting resin molding
US4902215A (en) * 1988-06-08 1990-02-20 Seemann Iii William H Plastic transfer molding techniques for the production of fiber reinforced plastic structures
US4942013A (en) * 1989-03-27 1990-07-17 Mcdonnell Douglas Corporation Vacuum resin impregnation process
US5052906A (en) 1989-03-30 1991-10-01 Seemann Composite Systems, Inc. Plastic transfer molding apparatus for the production of fiber reinforced plastic structures
JP2947866B2 (ja) * 1990-04-20 1999-09-13 富士重工業株式会社 複合材の成形方法および成形装置
US5403537A (en) * 1993-09-14 1995-04-04 Martin Marietta Corporation Method for forming composite structures
JP3483623B2 (ja) 1994-07-19 2004-01-06 富士重工業株式会社 繊維強化プラスチック構造部材の成形方法
US5565162A (en) * 1994-09-30 1996-10-15 Composite Manufacturing & Research Inc. Method for manufacturing a fiber reinforced composite article
US5576030A (en) 1995-10-02 1996-11-19 Lockheed Corporation Apparatus for fabricating composite parts
GB9616455D0 (en) * 1996-08-05 1996-09-25 Short Brothers Plc Apparatus and method for forming a fibre reinforced resin composite component
US5968445A (en) * 1998-01-05 1999-10-19 The Boeing Company Method and apparatus for curing large composite panels
JP3994552B2 (ja) 1998-11-12 2007-10-24 東レ株式会社 Ｆｒｐ製屋根材およびその製造方法
US6555045B2 (en) 1999-01-11 2003-04-29 Northrop Grumman Corporation Grooved mold apparatus and process for forming fiber reinforced composite structures
US7081219B2 (en) * 1999-03-18 2006-07-25 Stewart David H Method and machine for manufacturing molded structures using zoned pressure molding
JP3410462B2 (ja) * 1999-06-28 2003-05-26 旭ファイバーグラス株式会社 長繊維強化熱可塑性樹脂成形体の製造方法及びそれによる製造物
JP2001064406A (ja) * 1999-08-31 2001-03-13 Toray Ind Inc 繊維強化複合材用プリフォームおよびこれを用いてなる繊維強化複合材ならびにこれらの製造方法
GB2360483A (en) * 2000-03-02 2001-09-26 Slingsby Aviat Ltd Improvements in the manufacture of resin-impregnated components
DE10013409C1 (de) * 2000-03-17 2000-11-23 Daimler Chrysler Ag Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens
US6818159B2 (en) 2000-03-17 2004-11-16 Deutsches Zentrum Fuer Luft-Und Raumfahrt E.V. Process for the production of a composite consisting of a fiber reinforced material
JP4609745B2 (ja) * 2000-12-06 2011-01-12 東レ株式会社 Ｆｒｐの真空成形方法
US6630095B2 (en) * 2001-08-01 2003-10-07 Lockheed Martin Corporation Method for making composite structures
DE10140166B4 (de) * 2001-08-22 2009-09-03 Eads Deutschland Gmbh Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens
US7189345B2 (en) * 2003-08-13 2007-03-13 The Boeing Company Method for vacuum assisted resin transfer molding

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
"MANUFACTURING PROCESSES FOR ADVANCED COMPOSITES", 1 January 2004, ELSEVIER ADVANCED TECHNOLOGY, OXFORD, GB, ISBN: 978-1-85617-415-2, article FLAKE C. CAMPBELL: "Vacuum-assisted Resin Transfer Molding", pages: 349 - 353, XP055409067 *

Also Published As

Publication number Publication date
EP2644365A2 (fr) 2013-10-02
ES2628600T3 (es) 2017-08-03
EP1555104B1 (fr) 2016-04-27
AU2008203839A9 (en) 2009-01-08
AU2008203841B2 (en) 2011-03-17
AU2003271139B2 (en) 2008-08-07
US20130207293A1 (en) 2013-08-15
EP2644363A2 (fr) 2013-10-02
AU2003271139A1 (en) 2004-05-04
EP1555104A1 (fr) 2005-07-20
AU2008203839A1 (en) 2008-09-04
WO2004033176A1 (fr) 2004-04-22
US9120253B2 (en) 2015-09-01
AU2008203841A1 (en) 2008-09-04
AU2008203840B2 (en) 2011-03-17
EP2644365A3 (fr) 2014-08-13
EP2644364A3 (fr) 2014-08-13
EP1555104A4 (fr) 2011-03-23
ES2727872T3 (es) 2019-10-21
US9463587B2 (en) 2016-10-11
US20060125155A1 (en) 2006-06-15
US8420002B2 (en) 2013-04-16
AU2008203840A1 (en) 2008-09-04
US20130228956A1 (en) 2013-09-05
EP2644363A3 (fr) 2014-08-13
EP2644364A2 (fr) 2013-10-02
AU2008203841A9 (en) 2009-01-08
EP2644363B1 (fr) 2017-03-22
US20130207316A1 (en) 2013-08-15
AU2008203839B2 (en) 2011-03-17

Similar Documents

Publication Publication Date Title
EP2644365B1 (fr) Méthode de moulage RTM
US20090252921A1 (en) Method for the production of a sandwich component having a honeycomb core and the sandwich component obtained in this way
US20050126699A1 (en) Process for the manufacture of composite structures
EP1595688B1 (fr) Stratifié moulé et son procédé de production
US8337740B2 (en) Reinforced internal composite structures
US8628709B2 (en) Method for producing a concave-shaped in particular U-shaped piece in a composite material and device for carrying out the same
JP2013504454A (ja) 複合材料の改良された製造方法及び製造装置
US20100139839A1 (en) Integral toolface breathing
JP2003025347A (ja) 真空ｒｔｍ成形方法
JP4104414B2 (ja) 繊維強化樹脂成形体の製造方法
JP2007176163A (ja) 繊維強化プラスチックの製造方法
JP4104413B2 (ja) Ｒｔｍ成形方法
ES2578930T3 (es) Método de moldeo de FRP

Legal Events

Date Code Title Description
17P Request for examination filed

Effective date: 20130711

AC Divisional application: reference to earlier application

Ref document number: 1555104

Country of ref document: EP

Kind code of ref document: P

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): ES FR IT

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): ES FR IT

RIC1 Information provided on ipc code assigned before grant

Ipc: B29C 70/44 20060101AFI20140709BHEP

Ipc: B29C 70/54 20060101ALI20140709BHEP

17Q First examination report despatched

Effective date: 20160923

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20180601

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTC Intention to grant announced (deleted)
INTG Intention to grant announced

Effective date: 20181105

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AC Divisional application: reference to earlier application

Ref document number: 1555104

Country of ref document: EP

Kind code of ref document: P

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): ES FR IT

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2727872

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20191021

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20200103

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20210910

Year of fee payment: 19

Ref country code: FR

Payment date: 20210913

Year of fee payment: 19

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20211105

Year of fee payment: 19

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221031

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221009

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20231129

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221010

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221010